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FPGA development for high altitude subsonic parachute testingThis paper describes a rapid, top down requirements-driven design of an FPGA used in an Earth qualification test program for a new Mars subsonic parachute. The FPGA is used to process and store data from multiple sensors at multiple rates during launch, ascent, deployment and descent phases of the subsonic parachute test.
Document ID
20060042918
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Kowalski, James E.
Konefat, Edward H.
Gromovt, Konstantin
Date Acquired
August 23, 2013
Publication Date
September 1, 2005
Meeting Information
Meeting: Military and Aerospace Programmable Logic Device International Conference
Location: Washington, DC
Country: United States
Start Date: September 7, 2005
End Date: September 9, 2005
Distribution Limits
Public
Copyright
Other
Keywords
telemetry
FPGA methodology

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